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Distributed Finite Element Analysis Using a Transputer Network

机译:利用晶片机网络进行分布式有限元分析

摘要

The principal objective of this research effort was to demonstrate the extraordinarily cost effective acceleration of finite element structural analysis problems using a transputer-based parallel processing network. This objective was accomplished in the form of a commercially viable parallel processing workstation. The workstation is a desktop size, low-maintenance computing unit capable of supercomputer performance yet costs two orders of magnitude less. To achieve the principal research objective, a transputer based structural analysis workstation termed XPFEM was implemented with linear static structural analysis capabilities resembling commercially available NASTRAN. Finite element model files, generated using the on-line preprocessing module or external preprocessing packages, are downloaded to a network of 32 transputers for accelerated solution. The system currently executes at about one third Cray X-MP24 speed but additional acceleration appears likely. For the NASA selected demonstration problem of a Space Shuttle main engine turbine blade model with about 1500 nodes and 4500 independent degrees of freedom, the Cray X-MP24 required 23.9 seconds to obtain a solution while the transputer network, operated from an IBM PC-AT compatible host computer, required 71.7 seconds. Consequently, the $80,000 transputer network demonstrated a cost-performance ratio about 60 times better than the $15,000,000 Cray X-MP24 system.
机译:这项研究工作的主要目的是证明使用基于晶片机的并行处理网络以极具成本效益的方式加速有限元结构分析问题。该目的以商业上可行的并行处理工作站的形式实现。工作站是台式机尺寸的,低维护的计算单元,具有超级计算机的性能,但成本却降低了两个数量级。为了实现主要研究目标,采用了基于晶片机的结构分析工作站XPFEM,该工作站具有类似于商用NASTRAN的线性静态结构分析功能。使用在线预处理模块或外部预处理程序包生成的有限元模型文件被下载到32个晶片机的网络中以加速解决方案。该系统当前以大约三分之一的Cray X-MP24速度执行,但可能会出现额外的加速度。对于NASA选择的具有约1500个节点和4500个独立自由度的航天飞机主机涡轮叶片模型的演示问题,Cray X-MP24需要23.9秒才能获得通过IBM PC-AT运行的晶片机网络的解决方案兼容主机,需要71.7秒。因此,价值80,000美元的晶片机网络的性价比是1,500万美元Cray X-MP24系统的约60倍。

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